An agglomeration multigrid method was applied to numerical calculation of rotor forward flight flow based upon the unstructured dynamic overset grids.
基于非结构动态嵌套网格,将聚合多重网格方法引入到旋翼的前飞流场计算中。
An agglomeration multigrid method was applied to numerical calculation of rotor forward flight flow based upon the unstructured dynamic overset grids.
基于非结构动态嵌套网格,将聚合多重网格方法引入到旋翼的前飞流场计算中。
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